View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63203U 26145.35244478 +.00000000 +00000-0 +44681-3 0 00008
2 63203 43.0004 12.6288 0000934 246.8781 113.1972 15.27591532 00
| Epoch (UTC): | 25 May 2026 08:27:31 |
| Eccentricity: | 0.0000934 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.6288° |
| argument of perigee: | 246.8781° |
| revolutions per day: | 15.27591532 |
| mean anomaly at epoch: | 113.1972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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